STARLINK-34582, 64781
Orbit data source: Space-Track
STARLINK-34582, 64781 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 08 Jul 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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64781 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-34582
1 64781U 25147AC 26235.56945859 .00023203 00000-0 69575-3 0 9999
2 64781 53.1595 183.9293 0001413 85.3619 274.7545 15.34399555 64285Epoch: 2026-08-23T13:40Z
TLE epoch observation values (Epoch: 2026-08-23T13:40:01.222Z)
Latitude
-0°
Longitude
7.06058°
Altitude
463.526 km
Speed
7.636 km/s
True Right ascension
12h 15m 43s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:59:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.928 km
Perigee altitude
461.995 km
Semi-major axis
6,841.099 km
Eccentricity
0.00014
Inclination
53.1595°
RAAN
183.9293°
Arg. of periapsis
85.3619°
True anomaly
274.73836°
Mean anomaly
274.7545°
Eccentric anomaly
274.74643°
Mean motion
3.83579 °/min
Orbital period
93.85 mins
BSTAR
0.00069575
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Other satellites on launch #147 in the year 2025 (2025-07-08 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-34582 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-24 00:51:10.442Z | 283.382° WNW | 2026-08-24 00:54:10.442Z | 343.395° N | 20.236° | 2026-08-24 00:56:10.442Z | 21.501° NNE |
| 5 mins | 2026-08-24 05:48:10.442Z | 333.598° NNW | 2026-08-24 05:50:10.442Z | 57.363° ENE | 36.094° | 2026-08-24 05:53:10.442Z | 111.501° ESE |
| 5 mins | 2026-08-24 22:40:10.442Z | 200.116° SSW | 2026-08-24 22:42:10.442Z | 148.393° SSE | 34.729° | 2026-08-24 22:45:10.442Z | 65.182° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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